US2113335A - Bearing - Google Patents

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US2113335A
US2113335A US745381A US74538134A US2113335A US 2113335 A US2113335 A US 2113335A US 745381 A US745381 A US 745381A US 74538134 A US74538134 A US 74538134A US 2113335 A US2113335 A US 2113335A
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bearing
shaft
thrust
projections
air
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US745381A
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Wallgren August Gunn Ferdinand
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • F16C33/1025Construction relative to lubrication with liquid, e.g. oil, as lubricant
    • F16C33/106Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
    • F16C33/1075Wedges, e.g. ramps or lobes, for generating pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/08Elastic or yielding bearings or bearing supports, for exclusively rotary movement primarily for axial load, e.g. for vertically-arranged shafts

Description

April 5, 1938.
A. G. F. WALLGREN 2,113,335
BEARING 4 Sheets-Sheet 1 Filed Sept. 25, 1934 v J 4 ATTORNEY ya 6 BY ldca j April 1938. A. G. F. WALLGREN BEARING Filed Sept. 25, 1934 4 Sheets-Sheet 2 IN ENTOR @BY flju.
AT TgRNEY April 5, 1938.
A. G. F. WALLGREN BEARING Filed Sept. 25, 1954 4 Sheets-Sheet 3 I vENTdR @am M April 5, 1938. A. G. F. WALLGR EN 2,113,335
BEARING Filed Sept. 25, 1934 4 Sheets-Sheet 4 fin.
INVENTg M W 9 fin'onuav Patented Apr. 5, i938 UNITED SATES PATENT OFFICE BEARING Application September 25, 1934, Serial No. 745,381 In Germany September 29, 1933 11 Claims.
My invention relates to bearings, and more particularly to bearings of both radial and thrust types which are arranged for lubrication by air or any other suitable gas.
The lubrication of any bearing in which sliding surfaces are employed is effected through the medium of a film of lubricant which is maintained between the surfaces by reason of the rotation of one of them. This film acts to prevent actual metal-to-metal contact between the surfaces, thereby reducing friction and wear. In a welllubricated bearing the friction that is produced is within the lubricating film itself. The value of this friction depends upon the viscosity of the lubricant and increases with an increase in viscosity. Inasmuch as air or any other gas has a much lower viscosity than any liquid, the friction produced in an air lubricated bearing will be much less than in a bearing lubricated by oil or other liquids.
Due to the low viscosity of gas, it has heretofore been considered to be impossible to satisfactorily lubricate bearings unless the gas is fed to the bearing surfaces under comparatively high pressures. Even in these cases, the gas under pressure has not usually been employed as a lubricant in the true sense of the word, but has been used to support the major part of the load, and to thus relieve ordinary oil-lubricated bearings to this extent.
In order to satisfactorily lubricate a bearing with air under pressure which differs from that of the surrounding atmosphere only by an amount resulting from the rotation of the bearing itself, I have found that comparatively high bearing speeds are necessary. Moreover, the bearing surfaces should be accurately machined and as free as possible from scratches and the like. Also, due to the fact that no oil whatsoever is employed, the bearing surfaces must be of a material which will not rust when exposed to the moisture in the air. I have found that iron or steel with additions of nickel or chromium in compositions which permit the hardening of thematerial, are very satisfactory metals. Also, the bearing surfaces may be nickel or chromium plated in order to prevent rusting, or moisture resisting artificial resin, such, for example, as Bakelite, may be employed as well as cellulose products, such as Cellon.
In order that the thin air film should not be disrupted, it is important that the bearing surfaces should be in accurate alignment so as to prevent concentration of the load at one or two points. With oil lubricatiombearing alignment can be easily obtained by making the bearing surfaces spherical. However, I have found that spherical bearing surfaces for air lubrication are not satisfactory, due apparently to the fact that tendencies toward axial displacement, caused by axial thrust, which is unavoidable, concentrate the load at a limited area. In order to overcome this difiiculty, I have found it best to employ cylindrical bearing surfaces for radial bearings, so that a slight axial displacement of one surface with respect to the other has no adverse effeet and to allow for alignment of the surfaces by mounting one of the bearing members on a universal joint arrangement whereby it may remain in perfect alignment with the other bearing member. Such a universal joint should be perfectly free to allow universal movement of the bearing member supported thereby with a minimum amount of frictional resistance and still be capable of supporting the load in a radial direction. For thrust bearings, I have found that substantially fiat surfaces are best. As is the casewith radial bearings, one of the bearing members should be mounted for universal movement to allow for misalignment of the shaft. 25
Bearings in accordance with the present invention have been successfully applied to spindles for spinning mills. These spindles have been operated at approximately 12,000 R. P. M. continuously over a period of many months. No wear in the sliding surfaces could be ascertained, even with delicate precision instruments, and the power required to operate them was much less than with oil lubricated bearings. Likewise, the temperatures developed by the air lubricated bearings were substantially below those in oil lubricated bearings for the same purpose.
Further objects and advantages of my invention will be apparent from the following description considered in connection with the accompanying drawings which form a part of this specification and in which:
Fig. 1 is a view partly in cross-section, of a spinning spindle structure in accordance with my invention;
Fig. 2 is a cross-sectional view on an enlarged scale taken on the line 2--2 of Fig. 1;
Fig. 3 is a view similar to Fig. l, but showing a somewhat modified embodiment of my invention;
Fig. 4 is a cross-sectional view taken on the line 4-4 of Fig. 3:
Fig. 5 is a cross-sectional view taken on the line 55 of Fig. 4;
Fig. 6 is a cross-sectional view taken on the line 56 of Fig. 4;
Fig. 7 is a top view of a ring element employed in the bearing shown in Figs. 3 through 6;
Figs. 8 through 18 show various forms of thrust bearings which may advantageously be employed in the spinning spindles shown in Fig. l or Fig. 3;
Fig. 19 is a cross-sectional view of an air lubricated thrust bearing;
Fig. 20 is a top view of a bearing member employed in Fig. 19;
Fig. 21 is a cross-sectional view taken on the line 2i--2I of Fig. 20;
Fig. 22 is a top view of a Cardan ring employed in the bearing shown in Fig. 19;
Fig. 23 is a cross-sectional view taken on the line 23-23 of Fig, 22;
Fig. 24 is a cross-sectional view showing another embodiment of air lubricated thrust bear- Fig. 25 is a view, similar to Figs. 1 and 3. but of a still different embodiment of my invention; and
Fig. 26 is a cross-sectional view of my invention as applied to a vacuum cleaner.
Referring more particularly to Figs. 1 and 2. reference character I l designates the upper portion of a vertical shaft of a spinning spindle. The lower portion of the shaft is designated by reference character I2, and the two portions are joined together by a bushing 13. The lower end of portion 12 is tapered, as shown at I4, to form a thrust bearing member, which turns on the thrust member l5. Rigidly secured to the upper portion ll of the shaft by means of a rivet or the like is a pulley 16 formed with a hollow portion. The inner surface of this hollow portion is accurately machined to cylindrical form to provide the rotating member of the bearing surfaces IT. The diameter of this bearing surface is preferably made as large as the space conditions will permit, in order that it may have as high 11 peripheral speed as is possible. Consequently, this cylindrical surface is placed as close as possible to the bottom of the pulley groove lfia. Likewise. the center of the pulley groove is located equidistant from the ends of the bearing surface, so that the radial pull on the pulley resulting from the driving belt will be applied at the center of the surface.
In the annular space between the shaft H and the hollow portion of the pulley Hi, there extends a stationary sleeve 18, the inner diameter of which is greater than the diameter of the shaft, so that no contact between the two takes place. Sleeve 18 is provided with diametrically opposed recesses which receive the inner ends of pins l9, as is clearly shown in Fig. 2. The outer ends of pins I!) are received in recesses formed in a Cardan ring 20. The ring 20 may comprise a single ring. or it may be made up of a plurality of concentric rings. Inasmuch as ring 20 should be somewhat resilient for purposes of assembly, it is preferable to use several concentric rings in order to provide this resiliency while giving the ring sufficient strength in radial direction. Disposed at 90 from the openings which receive pins l9. ring 20 is provided with openings which receive the inner ends of similar pins 21. The outer ends of pins 2| are received in recesses formed in a cylindrical member 22, which member forms the inner stationary bearing member. Its outer cylindrical surface is accurately machined and cooperates with the inner cylindrical surface of hollow pulley l6. Pins l9 and 2| are formed with intermediate collars 24, the purpose of which is to space the Garden ring 20 from both the sleeve l8 and the bearing member 22 and to prevent radial play between those members.
Sleeve I8 is rigidly supported in a standard 25, which may be clamped to a bench or the like by means of a nut 25 threaded thereon. Also threaded on standard 25 is a housing 23, which encloses a lower bearing. This bearing is similar to the one described above, except that the Cardan ring 20a is located between the rotating bushing l3 and the rotating bearing member 22a instead of between the stationary sleeve l8 and the stationary bearing member 22. The inner surface of housing 23 is accurately machined to cylindrical form and provides the stationary member of the bearing surfaces ll. Thrust block I5 may be threaded into the lower end of housing 23.
An arm 27 is pivotally supported on standard 25 and is provided with a hook-shaped member 28 overhanging a portion of the pulley l6. When a bobbin is pulled off the spindle shaft II it may tend to pull the shaft and associated parts with it. Such movement causes the pulley to engage member 28 and causes the latter to tend to rotate arm 21 in a counter-clockwise direction,
which rotation is prevented by the arm being in contact with standard 25. However, if it is desired to remove the shaft ll, arm 21 may be pivoted in a clockwise direction so as to move member 28 out of the path of the pulley.
The lower end of hollow pulley H5 is formed as an outwardly flared conical flange I61) which rotates close to a conical projection 25!) formed on standard 25. The upper end of the pulley is closed by shaft H.
The operation of the above described device is as follows:
In Fig. 2 there is shown in an exaggerated manner the relative positions of the rotating bearing surface on pulley l6 and the stationary bearing surface of member 22 during rotation of the former in the direction indicated by the arrow a. assuming the resultant radial load imposed on the shaft H by the pull of the cord driving the pulley and the pull of the thread being wound on the bobbin to be in the direction indicated by the arrow 2). In practice, the clearance between the bearing surfaces is approximately 0.001 of an inch, the diameter of the bearing surfaces being one inch. The rapid rotation of the cylindrical surface on the pulley l6 causes air to be rotated therewith, and this air is compressed somewhat between the bearing surface on pulley l6 and that on stationary member 22 at the region where the radial load acts to bring these surfaces into contact. The result is that a thin film of air is maintained between the surfaces, this air being at a pressure above that of the surrounding air, this increase in pressure resulting solely from the rotation of the pulley Hi. It will be noted that no other means whatsoever'is provided for forcing air between the bearing surfaces. The operation of the bearing at the lower end of the shaft is exactly the same as that above described. except that member 22a rotates and builds up the film of air.
In the event that shaft II is slightly out of alignment, the bearing surface on pulley IE will have a slight wobbling motion. If stationary bearing member 22 were rigidly fixed, this would result in concentrated bearing pressures near the ends of member 22, which would have a tendencyto cause the bearing to bind and disrupt the air film. However, due to the fact that member 22 is mounted so as to have universal move ment with respect to fixed sleeve l8, member 22 tween the bearing surfaces.
may participate in this wobbling motion with the result that there is no relative wobbling be- This gives an even distribution of bearing pressure and prevents the breaking down of the air film. The same is true with respect to the lower hearing, but in this case the stationary bearing surface of fixed member 23 cannot wobble, and the rotating member 22a is able to run true with respect to the stationary surface, even though the shaft wobbles, by virtue of the fact'that it is mounted for universal movement with respect to the shaft. The thrust load on the shaft, resulting from its weight, as well as that of the bobbin mounted on the upper end thereof, is carried by the thrust bearing including members l4 and I5.
The lower bearing being completely enclosed, there is no opportunity for foreign matter, such as dust particles to get to the bearing surfaces. The entrance of foreign matter to the bearing surfaces of the upper bearing is prevented by the conical flange i6b on the pulley i6, which rotates close to the conical projection 251) on the standard 25. The rotation of the conical flange l6b causes air to rotate in the space between it and projection b with the result that any particles which tend to enter through this space are caught up by the rotating air and thrown outwardly by centrifugal force.
The embodiment shown in Figs. 3 through differs from that .just described only in the manner. of mounting the bearing members for uni- .metrically opposed outward projections 3|, the
latter disposed at 90 with respect to the former. Projections 82 are clamped between clamping rings 35 and 36, as clearly shown in Fig. 6. R0- tating bearing member 22 is providedwithinternal clamping rings 33 and 34, which serve to clamp between them the outward projections 3| of the discs 30. Clamping rings a and 24 may be retained in place bythreaded lock rings 31, and clamping rings 35 and may be retained in place by a locking ring 38. As shown, ring 38 is not threaded, but is forced onto sleeve ll with a driving fit. Obviously this ring could be threaded in the manner shown in connection with lock rings 31, or the latter could be retained in place by a driving fit.
In order to prevent relative rotation between the discs on the one hand and the sleeve II or bearing member 22 on the other, clamping rings 34 and 36 are provided with projections 24a and 36a, respectively, at the portions of their circumferences which do not engage the projections 2i and 32. respectively, on the discs 20.
These projections are not as long as the total thickness of the disc bundler because if they'were they might contact rings 33 and 35, respectively,
and thus prevent the clamping rings from clamp- 7 the lower end of shaft l2 conical.
38a on the clamping ring and the projections 32 on the discs is very small, as indicated by the distance 0. The-same is true with respect to the projections 34a on the clamping rings and the projections 3| on the discs.
This embodiment operates in the same manner as that described in connection with Figs. 1 through 3, except that the universal movement of the bearing member 22 with respect to the fixed I sleeve l8 results from the resiliency of the discs 30. Due to the fact that thereis'no play between any of the parts, as there is bound to be with respect to the pins l9 and 2| shown in Fig. 2, no wear can take place, and hence theuniversal joint arrangement cannot becoine loose.
The lower bearing on the spindle shown in Fig. 3 is'similar to the upper one, except that the bearing member 22a carried by the discs 30- rot'ates with the shaft, while the outer bearing member is fixed. In this respect it is the same as the lower bearing shown in Fig. .1. v
In order to avoid undue strain on the discs 30.
collars 38a are provided on the inner clamping rings 38 and serve to limit the amount of universal movement between the bearing members supported by the rings and the members which support the rings.
Figs. 8 through 18 show various forms of thrust bearings which may be used in conjunction with the spinning spindles shown in either Figs, 1 or 3. In Fig. 8 the thrust bearing is formed by making The point of the cone rotates on the thrust member i5. As a matter of practice, it is impossible to make the parts accurately enough so that the center of the shaft l2 coincides exactly with the center of the bearing. The distance between these two center lines is shown in exaggerated form in Fig.
'8 and designated by reference character d.
However, inasmuch as the lower end of shaft i2 is formed as a point this point can travel in a small circle on the thrust member I5, thus allowing for inaccuracies in the alignment of the center of the shaft with respect to the center of the bearing.
/ After continued use the conical end of the shaft will wear a slight depression in the thrust member ii. The small particles of metal thus worn off the shaft and the thrust member will collect in this depression and actas an abrasive and thus aggravate the wear. ,In order to over- .come this drawback the construction shown in Fig. 9 may be resorted to. As is clearly shown. the lower end of shaft I2 is flat and a conical point lia is formed on the thrust member I. Although the point I541 will tend to wear a depression in the end of the shaft, the small particles of metal will fall away from the wearing surfaces and hence will not act as an abrasive.
In the embodiment shown in Fig. 10 the thrust member I5 is formed with a conical recess lib in which the conical point on the shaft i2 turns. In the case of misalignment of, theshaft the conical end thereof can roll around, so to speak, the conical wall of recess lib, as is shown in Fig. 10. This construction, however, has the same drawback as that shown in Fig. 8 and an improvement thereover is shown in Fig. 11, where the thrust member I5 is formed with a conical projection lie and the conical recess is formed in thelower end of shaft l2. .Again, with this latterconstruction any particles of metal which are worn away will fall out of the recess.
In Fig. 12 the thrust member l5, instead of being rigidly secured to the lower bearing housing ref 23, is suspended therefrom by means of wires or other fiexible members 40. With this construction, the thrust member I5 is displaceable in a small circle together with the shaft if the latter is out of alignment with respect to the center of the bearing. Fig. 13 shows a top view of the thrust member 15 which is formed as an arbor with three arms and which is made as light as possible. In the modification shown in-Figs. 12 and 13 the thrust member is formed with a conical recess I51) and the lower end of the shaft is formed as a conical point.
In Fig. 14 the thrust member I5 is formed with a conical projection I 5a while the lower end of the shaft is formed with a conical recess for the same reasons as above pointed out. In this modification the wires 48 extend through slots or grooves 23a formed in the outer surface of bearing housing 23 and are thus protected from injury.
In the embodiment shown in Fig. 15 the lower end of shaft 12 is formed with a cylindrical recess and thrust member I5 is formed with a pinlike projection [5a. which extends into the cylindrical recess in the shaft. This construction has the advantage of reducing any tendency for the shaft to vibrate in an axial direction In the embodiment shown in Figs. 16 to 18, the thrust member is supported by the rotating radial bearing member 22a instead of directly by the lower end of shaft l2. As is shown in all of these figures, a plate 42 with a conical portion 43 is rigidly secured to the lower end of bearing member 22a. In Fig. 16 the wearing point 44 of conical member 43 is made of an exceptionally hard material, such as wolfram-tantalum-carbide, so called Widia-metal or titanite, or the like, and turns on a block 45 of similar material held by the bearing member l5. In Fig. 17 conical portion 43 is formed with a spherical end 44a which turns on block 45. In Fig. 18 spherical end 44a turns on spherical member 450. retained in thrust member [5.
The advantage of having the thrust-bearing secured rigidly to the rotary bearing member 22a,
instead of forming it as a part of the shaft 1!,
lies in the fact that .the rotary bearing member 22a and the thrust bearing can be secured together and then turned down or ground in a single operation, thus assuring perfect alignment of the axes of rotation of the two bearing .opp'osed projections 48 is retained in thrust member I5, the thrust member being formed with recesses to receive the projections. The 'upper side of Cardan ring 48 is formed with diametrically opposed projections 50 which are disposed at 90 with respect to projections 4a. Projections 50 engage in recesses 41b formed in the lower face of stationary thrust bearing member 41. Consequently bearing member 41 may have universal movement with respect to thrust member l5. The upper bearing surface of member 41 is formed with radial slits 41a. Rotation of bearing member 46 at a high speed causes an air film to be carried along thereby, the air finding access to the bearing surfaces through slits 41a, and this film prevents direct metal-to-metal contact between the bearing surfaces. The Cardan ring support 48 allows the stationary bearing member 41 to remain in perfect alignment with the rotating member 46 even though the shaft is slightly out of alignment and wobbles.
The embodiment shown in Fig. 24 is the same as that shown in Fig. 19 with the exception that the Cardan ring 48 is replaced by a ball 5| which engages spherical recesses in bearing member 41 and in thrust member 15. This ball and socket type of support permits universal movement of the bearing member 41 with respect to the thrust member.
In Fig. 25 there is shown a spinning spindle which is generally similar to that shown in Fig. l or 3. It diifers, however, in the fact that a hub 60 is secured to shaft H to which is riveted a pulley sleeve 6| formed with a pulley groove 62. The inner cylindrical surface of sleeve 6| is formed as a bearing surface and cooperates with the stationary bearing member 22. The forming of hub 60 and sleeve 6| as separate parts, instead of as an integral member l6, as shown in Fig. 1 or 3, makes the bearing surface more accessible for accurate machining. For the same reason the lower bearing housing 23 is not directly threaded on the standard 25 but is secured thereto by ,means of an intermediate sleeve 23a which is pressed or otherwise secured to the housing. Another difference resides in the fact that standard 25 is formed with an-integral cylindrical portion l8a, whereas in the previous modifications this member, designated by reference character I8, was separate. The construction and mode or operation of the air-lubricated bearings shown in Fig. 25is the same as that described in connection with Fig. 3, wherefore the description need not be' repeated.
Fig, 26 shows the application of air-lubricated bearings in accordance with my invention to the motor-fan unit of a vacuum cleaner. The vacuum cleaner includes anouter casing 52 within which motor-fan unit 53 is resiliently supported by means of springs 54 arranged at either end thereof. Armature shaft 55 of the motor is provided on either side of the armature, with cylindrical rotating bearing members 56. These members are made with as large a diameter as the space limitations will permit, in order to have as high a peripheral speed as is possible. Bear;- ing housings 51 are supported in either end of the motor housing. Stationary bearing members 59-are supported within bearing housings 5"! by means of a Cardan ring or the like 58 which, as illustrated, is similar to that shown in Figs. 1 and 2. However, any other suitable means for obtaining universal movement may be employed.
In operation, the bearing members 55 rotate with high peripheral speed and carry with them a thin film of air which is maintained between the outer bearing surfaces of members 56 and the inner bearing surfaces of members 59, thus preventing direct metal-to-metal contact between them. In the event that the shaft is slightly out of alignment, thus causing bearing members 55 purposes of illustration only and that the hearing may be applied to many other purposes. Also throughout the specification I have referred to air as a lubricant. It will be appreciated that any gas which does not have injurious effect upon materials of the bearings may be used instead of air. Finally, my invention is to be limited only by the appended claims viewed in the light of the prior art.
What I claim is:
1. A gas-lubricated bearing for sustaining the axial load on .a shaft including a disc-shaped bearing member having radialgrooves formed in the bearing surface thereof, means for securing said bearing member to said shaft, a bearing support, a second disc-shaped bearing member, and
means for connecting said second bearing mem-.
a plurality of resilient rings and having a pair of diametrically opposed projections on one side and another pair of diametrically opposed projections on the other side and disposed at 90 from the first pair and means for retaining one of said pairs of projections with respect to said element and for retaining the other of said pairs with respect to said member, and a second bearing member connected to the other of said elements.
3. In a bearing for relatively rotatable elements, a first bearing member, means for connecting said member to one of said elements, said means including a plurality of circular concentric resilient rings formed with recesses disposed 90 apart around the circumference, a pair of pins extending inwardly from diametrically opposed recesses and a pair -of pins extending outwardly from the other recesses, said element being formed with recesses to receive one of said pairs of pins and said member .being formed with recesses to receive the other pair, and a second bearing member connected to the other of said elements.
4. In a bearing for relatively rotatable elements, a first bearing member, means for connecting said member to one of said elements, said means including a resilient circular disc having a pair of diametrically opposed outward projections and a pair of diametrically opposed inward projections disposed at 90 to said outward projections, means for securing one of said pairs of projections to said element and means for securing the other pair to said member, and a second bearing member connected to the other of said elements.
5. In a. bearing for relatively rotatable elements, a first bearing member, means for connecting said member to one of said elements, said means including a plurality of resilient circular discs, each disc having a pair of diametrically opposed outward projections and a pair of difor clamping one of the pairs of aligned projections to said element and means for clamping the other pairs to said member, and a second bearing member connected to the other of said elements.
6. In a bearing for relatively rotatable elements, a first bearing member, means for connecting said member to one of said elements, said means including a plurality of resilient circular discs, each disc having apair ofdiametrically opposed outward projections and a pair of diametrically opposed inward projections disposed at 90 to said outward projections, similar projections on said discs being in alignment, means for clamping one of the pairs of aligned projections to said element and means for clamping the other pairs to said member, additional means for preventing relative rotation between said discs and said element and member, and a second bearing member connected to the other of said elements.
7. In a bearing for relatively rotatable elements, a first bearing member, means for connecting'said member to one of. said elements, said means including a plurality of resilient circular discs, each disc having a pair of diametricallyopposed outward projections and a pair of diametrically opposed inward projections disposed at 90 to said outward projections, similar projections on said disc's being in alignment, means for clamping one of the pairs of aligned projections to said element and means for clamping the other pairs to said member, stop means for limiting the universal movement possible between said element and said member, and a second bearing member connected to the other of said elements.
- 8. In a device of the class described, a rotatable shaft, a stationary bearing support, a radial bearing including a cylindrical bearing member secured to said bearing support, a second cylindrical bearing member, universal joint means 'for securing said second member to said shaft so as to maintain said second member in parallel alignment with said first member, said bearing members being arranged to be lubricated by air at a pressure which differs from atmospheric pressure by an amount resulting only from the rotation of the bearing, and a thrust bearing including a stationary thrust bearing element and flexible members for suspending said thrust bearing element from said bearing support.
9. A spinning-mill spindle including a vertical shaft, a stationary'support having a cylindrical portion surrounding and spaced from said shaft, 3, first cylindrical bearing member supported on the outside of said cylindrical portion, a hollow pulley secured to said shaft and having a portion surrounding said first bearing member, the interior of said portion of said pulley being formed as a cylindrical bearing surface cooperating with the bearing surface of said first bearing member, said bearing surfaces being arranged to be held out of metalto-metal contact during rotation by a film of air maintained therebetween by the rotation of said second bearing member, and a conical part on said stationary support, said hollow pulley being closed at one end and formed with a conical opening at the other positioned so as to rotate in proximity to said conicakpart, whereby foreign matter is excluded from said bearing member.
10. In a gas-lubricated bearing for relatively rotatable elements, a first bearing member, means for connecting said member to one of said elements, said means including a fiat circular disc of resilient material having a radial extent many times greater than its thickness whereby the disc is substantially rigid with respect to loads acting in a radial plane while being resiliently yieldable to forces acting in other planes, means for securing said disc at diametrically opposed points to said element, means for securing said disc to said member at diametrically opposed points disposed at 90 from the first mentioned points, and a second bearing member connected to the other of said elements, said bearing members being arranged to be separated during rotation by a film of gas maintained therebetween by rotation of one of said members.
11. In a bearing for relatively rotatable elements, a first bearing member, a resilient annular disc for connecting said member to one of AUGUST GUNNAR FERDINAND WALLGREN.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2531098A (en) * 1945-12-28 1950-11-21 Gen Electric Driving mechanism
US2684877A (en) * 1949-10-18 1954-07-27 Schneider Ernst Bearing
US2788249A (en) * 1953-06-18 1957-04-09 Joseph D Christian Bearing support and seal for shaft
US3022935A (en) * 1958-01-13 1962-02-27 Bristol Siddeley Engines Ltd Gas bearings
US3325231A (en) * 1963-10-10 1967-06-13 Webcor Inc Miniature motor bearing
US3394971A (en) * 1965-07-09 1968-07-30 Rolls Royce Bearing
US20150098844A1 (en) * 2013-10-09 2015-04-09 Compal Electronics, Inc. Fan module

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2531098A (en) * 1945-12-28 1950-11-21 Gen Electric Driving mechanism
US2684877A (en) * 1949-10-18 1954-07-27 Schneider Ernst Bearing
US2788249A (en) * 1953-06-18 1957-04-09 Joseph D Christian Bearing support and seal for shaft
US3022935A (en) * 1958-01-13 1962-02-27 Bristol Siddeley Engines Ltd Gas bearings
US3325231A (en) * 1963-10-10 1967-06-13 Webcor Inc Miniature motor bearing
US3394971A (en) * 1965-07-09 1968-07-30 Rolls Royce Bearing
US20150098844A1 (en) * 2013-10-09 2015-04-09 Compal Electronics, Inc. Fan module

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